| Type of Document |
Dissertation |
| Author |
Lawton, John Arthur
|
| URN |
etd-10142005-135753 |
| Title |
Fuel-optimal space-flight transfer solutions through a redundant adjoint variable transformation |
| Degree |
PhD |
| Department |
Aerospace Engineering |
| Advisory Committee |
| Advisor Name |
Title |
| No Advisors Found |
|
| Keywords |
- Space vehicles
- Propulsion systems
- Research
|
| Date of Defense |
1991-04-05 |
| Availability |
unrestricted |
Abstract
A transformation between minimum dimension adjoint variables and redundant adjoint
variables is derived in this dissertation. The transformation is then applied between the adjoint
variables associated with Cartesian position and velocity vectors and a set of redundant adjoint
variables associated with certain regularized variables (Schumacher variables). This
transformation proves to be very beneficial when it is applied to minimum-fuel space rendezvous
and intercept problems. It facilitates using attributes from the two systems simultaneously; a
new necessary condition in Schumacher adjoints is derived in this dissertation, and this together
with classical necessary conditions for fuel-optimal transfer (existing in the position and velocity
space) leads to a numerical algorithm which seems to be quite robust in finding candidate
optimal control solutions for space transfer problems.
|
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LD5655.V856_1991.L387.pdf |
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